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作 者:徐铧东 于东[2] 刘文翔 石景富 苗常青[1] XU Huadong;YU Dong;LIU Wenxiang;SHI Jingfu;MIAO Changqing(National Key Laboratory of Science and Technology on Advanced Composites in Special Environments,Harbin Institute of Technology,Harbin 150001,China;Department of Mechanical Design,School of Mechanical and Electrical Engineering,Harbin Institute of Technology,Harbin 150001,China)
机构地区:[1]哈尔滨工业大学特种环境复合材料技术国家级重点实验室,哈尔滨150001 [2]哈尔滨工业大学机电学院机械设计系,哈尔滨150001
出 处:《载人航天》2022年第1期75-80,共6页Manned Spaceflight
基 金:载人航天领域预先研究项目(040101)。
摘 要:为提高航天器空间碎片防护结构的防护性能,减小其发射体积,提出了一种可折叠发射的屏间充气展开式多屏防护结构,通过充气展开支撑管在轨充气展开,成型为多屏大间距防护结构。分析了展开式多屏防护结构的空间碎片防护性能,得到了屏间距对多屏结构防护性能的影响规律。结果表明:在相同面密度下,展开式多屏防护结构的防护性能显著优于单屏防护结构,且其防护性能随屏间距的增大而提高。To improve the protective performance of the spacecraft space debris protective structure and to reduce the launch volume,an inflatable deployment multi-shield protective structure that could be launched in folded state was proposed.It could be deployed to an inflated multi-shield and large-spacing protective structure on-orbit.The space debris protective performance of the inflatable deployment multi-shield protective structure was analyzed and the influence of the shield spacing on the protective performance of the multi-shield structure was obtained.The results showed that the protective performance of the inflatable deployment multi-shield protective structure was significantly better than that of the single-shield protective structure under the same surface density,and the protective performance increased with the increase of the shield spacing.
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